Photonic devices having degenerate spectral band edges and methods of using the same

ABSTRACT

Provided herein are photonic devices configured to display photonic band gap structure with a degenerate band edge. Electromagnetic radiation incident upon these photonic devices can be converted into a frozen mode characterized by a significantly increased amplitude, as compared to that of the incident wave. The device can also be configured as a resonance cavity with a giant transmission band edge resonance. In an exemplary embodiment, the photonic device is a periodic layered structure with each unit cell comprising at least two anisotropic layers with misaligned anisotropy. The degenerate band edge at given frequency can be achieved by proper choice of the layers&#39; thicknesses and the misalignment angle. In another embodiment, the photonic device is configured as a waveguide periodically modulated along its axis.

This invention was made with Government support under grant numberFA9550-04-1-0359, awarded by Air Force Office of Scientific Research,Air Force Materials Command, USAF. The Government has certain rights tothis invention.

FIELD OF THE INVENTION

The invention relates generally to the field of photonic devices, andmore particularly to systems and methods for transmitting and storingelectromagnetic radiation in a photonic device with inhomogeneousspatially periodic structure.

BACKGROUND INFORMATION

The manipulation of electromagnetic energy can be advantageous tonumerous applications within many industries. For instance, much efforthas been focused on reducing the velocity of electromagnetic energy,such as light and microwave pulses. The reduced velocity ofelectromagnetic energy can facilitate manipulation of electromagneticwaves. It can also enhance the light-matter interaction essential innumerous optical and microwave applications. One approach to reducingthe electromagnetic energy velocity is through the use of spatiallyinhomogeneous periodic media displaying strong spatial dispersion atoperational frequencies. Spatial inhomogeneity results in strongnonlinear relation between the frequency ω of propagatingelectromagnetic wave and the respective Bloch wave number k. Therelation ω(k) is referred to as dispersion relation or, equivalently, ask-ω diagram. At certain frequencies, the wave group velocity v=dω/dkvanishes implying extremely low energy velocity.

One common photonic device exploiting spatial inhomogeneity is aphotonic crystal. This device is typically composed of multiplerepeating segments (unit cells) arranged in a periodic manner.Electromagnetic frequency spectrum of a typical photonic crystaldevelops frequency bands separated by forbidden frequency gaps. Thefrequency separating a photonic band from adjacent photonic gap isreferred to as a (photonic) band edge, or simply a band edge. Atfrequencies close to a photonic band edge, the relationship between thefrequency ω and the wave number k can be approximated asω−ω_(g)∝(k−k_(g))²  (1)implying that the respective group velocityv=dω/dk∝k−k _(g)∝√{square root over (ω−ω_(g))}  (2)vanishes as ω approaches the band edge frequency ω_(g). This createsconditions for very slow pulse propagation. Another common photonicdevice exploiting spatial inhomogeneity and providing conditions forslow energy propagation is a periodic array of weakly coupledresonators. There exist many different physical realizations of theindividual resonators connected into the periodic chain.

One common drawback of current photonic devices employing spatialinhomogeneity is that only a small fraction of the incidentelectromagnetic radiation is converted into the slow electromagneticmode, resulting in low efficiency of the device. Another common drawbackof current photonic devices is the necessity to employ a large number ofthe said segments (unit cells) in order to achieve a desirable slowdownof electromagnetic energy. Accordingly, improved photonic devices areneeded having smaller dimensions and allowing for more efficientmanipulation of the incident electromagnetic radiation.

SUMMARY

The devices, systems and methods described in this section are done soby way of exemplary embodiments that are not intended to limit thesedevices, systems and methods in any way.

In one exemplary embodiment, a photonic system is provided that includesa photonic device configured to display a degenerate band edge, thephotonic device including a first end, a second end, a first surfacelocated on the first end and a plurality of segments coupled togetherbetween the first and second ends. Each segment can include a firstanisotropic layer, a second anisotropic layer misaligned with the firstanisotropic layer, and a third layer. The photonic device can beconfigured to convert an electromagnetic wave incident on the firstsurface into a frozen mode, where the electromagnetic wave operates at afrequency in proximity with the degenerate band edge.

In another exemplary embodiment, a photonic system is provided thatincludes a photonic device configured to display a degenerate band edge,the photonic device including a first end, a second end, a first surfacelocated on the first end and a plurality of periodic segments coupledtogether between the first and second ends. Each segment can include afirst anisotropic layer having a first thickness and a secondanisotropic layer misaligned with the first anisotropic layer and havinga second thickness different from the first thickness. The photonicdevice can be configured to convert an electromagnetic wave incident onthe first surface into a frozen mode, when the electromagnetic waveoperates at a frequency in proximity with the degenerate band edge.

Other systems, methods, features and advantages of the invention will beor will become apparent to one with skill in the art upon examination ofthe following figures and detailed description. It is intended that allsuch additional systems, methods, features and advantages be includedwithin this description, be within the scope of the invention, and beprotected by the accompanying claims. It is also intended that theinvention not be limited to the details of the example embodiments.

BRIEF DESCRIPTION OF THE FIGURES

The details of the invention, including fabrication, structure andoperation, may be gleaned in part by study of the accompanying figures,in which like reference numerals refer to like parts. The components inthe figures are not necessarily to scale, emphasis instead being placedupon illustrating the principles of the invention. Moreover, allillustrations are intended to convey concepts, where relative sizes,shapes and other detailed attributes may be illustrated schematicallyrather than literally or precisely.

FIGS. 1-2 are block diagrams depicting exemplary embodiments of aphotonic device.

FIGS. 3A-D are graphs depicting exemplary k-ω diagrams of embodiments ofthe photonic device described with respect to FIG. 1 corresponding todifferent geometrical parameters of the photonic device.

FIGS. 4A-C are block diagrams depicting performance of an exemplaryembodiment of the photonic device in the frozen mode regime atfrequencies close to the degenerate band edge.

FIG. 5 is a graph depicting an exemplary frozen mode profile atsteady-state regime.

FIG. 6 is a graph depicting the profile of a typical electromagneticsurface wave at the air/photonic crystal interface of a photonic device.

FIG. 7 is a graph depicting an exemplary profile of an abnormal surfacewave at a frequency close to that of the degenerate band edge in anexemplary embodiment of the photonic device.

FIGS. 8-9 are graphs depicting performance of an exemplary embodiment ofthe photonic device in the regime of giant transmission band edgeresonance.

FIGS. 10-15C are block diagrams depicting additional exemplaryembodiments of a photonic device displaying degenerate photonic bandedge.

DETAILED DESCRIPTION

Photonic devices and systems having degenerate spectral band edges andmethods for using the same are described herein. These devices, systemsand methods are based on the physical idea of using spatially periodicstructures displaying a degenerate band edgeω−ω_(d)∝(k−k_(d))⁴  (3)rather then the regular band edge described by equation (1). Unlike theregular band edge (1), display of the degenerate band edge (3) allowsfor the frozen mode regime, accompanied by a complete conversion of theincident radiation into a slow mode with a drastically enhancedamplitude. In addition, a resonance cavity incorporating a photonicdevice displaying a degenerate band edge can have much smaller relativedimensions compared to those incorporating existing photonic devices.

Light transmitting periodic structures that can be configured to displaythe degenerate band edge (3) include, but are not limited to: (i)photonic crystals, such as periodic layered structures, as well asstructures with two and three dimensional periodicity, (ii) spatiallymodulated optical and microwave waveguides and fibers, and (iii) arraysof coupled resonators. The embodiments discussed below are directedtowards periodic arrays of anisotropic dielectric layers; however, it isimportant to emphasize that the underlying reason for the enhancedperformance of the photonic device as described herein lies in theexistence of a degenerate band edge (3) in the respective frequencyspectrum. Specific physical realization of the periodic structuredisplaying such a spectrum is determined by practical needs, i.e., oneof ordinary skill in the art will readily recognize how to implementspatially modulated optical and microwave waveguides and fibers, arraysof coupled resonators and other desired structural configurations basedon the embodiments described herein.

FIG. 1 is a block diagram depicting one exemplary embodiment of aphotonic device 101 configured to display a degenerate spectral bandedge (3). FIG. 1 depicts an electromagnetic wave 102 incident a surface111 of device 101. In this embodiment, photonic device 101 includes aplurality of segments (unit cells) 105 coupled together between a firstend 103 and a second end 104 of the device 101. Each segment 105 caninclude a first anisotropic layer 106, a second anisotropic layer 107,and a third optional layer 108. The third layer 108 can be made ofeither isotropic or anisotropic material, or it can be omitted entirely.The Z direction is normal to layers 106-108. The thickness of segment105 in the Z direction is preferably of the same order of magnitude asthe wavelength of the incident wave 102. Each of the three layers106-108 has a plane-parallel configuration with a uniform thickness(measured in the Z direction) and composition, although these conditionsmay not be necessary. The thickness of each of layers 106-108 can bedifferent from each other in accordance with the needs of theapplication.

In this embodiment, the structure of photonic device 101 is periodicalong the Z direction perpendicular to layers 106-108, which areparallel to the X-Y plane. The X, Y and Z directions are perpendicularto each other like that of a standard Cartesian coordinate system.Photonic device 101 is also preferably homogeneous in the in-planedirections X and Y, although photonic device 101 can also beinhomogeneous in the directions X, Y, or both, if desired. The totalnumber N of repeating segments 105 in photonic device 101 depends on thespecific application and usually varies between three and severalhundred, although device 101 is not limited to this range of segments105.

The anisotropy axes of anisotropic layers 106 and 107 preferably havemisaligned orientation in the X-Y plane with the misalignment angle φbeing different from 0 and π/2. In this embodiment, anisotropic layers106 and 107 are composed of the same anisotropic dielectric material andhave a variable misalignment angle. The dielectric permittivity tensorsof the three constitutive layers 106, 107 and 108 can be chosen asfollows:

$\begin{matrix}{{ɛ_{A\; 1} = \begin{bmatrix}{ɛ + \delta} & 0 & 0 \\0 & {ɛ - \delta} & 0 \\0 & 0 & ɛ_{zz}\end{bmatrix}},{ɛ_{A\; 2} = \begin{bmatrix}{ɛ + {{\delta cos}\; 2\varphi}} & {{\delta sin}\; 2\varphi} & 0 \\{{\delta sin}\; 2\varphi} & {ɛ - {{\delta cos}\; 2\varphi}} & 0 \\0 & 0 & ɛ_{zz}\end{bmatrix}},{ɛ_{B} = \begin{bmatrix}1 & 0 & 0 \\0 & 1 & 0 \\0 & 0 & 1\end{bmatrix}},} & (6)\end{matrix}$where ∈_(A1), ∈_(A2) and ∈_(B), are the dielectric permittivity tensorsfor the layers 106, 107 and 108, respectively. The choice (6) for thematerial tensor ∈_(B) corresponds to the case where layer 108 is anempty gap between the adjacent pairs of anisotropic layers 106 and 107.If desired, optional layer 108 can also be filled with eitheranisotropic or isotropic material, such as glass, air, active ornonlinear medium, etc., or it can be left vacant (e.g., as a vacuum),depending on the specific practical needs of the application. Thequantity δ in (6) describes inplane anisotropy of the A-layers 106 and107, essential for the existence of degenerate band edge. The parameterφ in (6) designates the misalignment angle between anisotropic layers106 and 107. It can be chosen anywhere between 0 and π, which providesadditional tunability of the photonic device. The k-ω diagram of thephotonic device in FIG. 1 can develop degenerate band edge (3) only ifthe misalignment angle φ is other than 0 and π/2. A typical value forthe misalignment angle φ is π/4. If desired, the tensor anisotropy (6)of layers 106 and 107 can be replaced with similar shape anisotropy ofthe respective X-Y cross sections, i.e., anisotropy can be induced withonly isotropic materials through the shape or configuration of the X-Ycross section of the respective layers (e.g., the X-Y cross section isshaped as a, rectangle, ellipse or the like). Additional exemplaryembodiments with modulated X-Y cross-sections are described with respectto FIGS. 10-13.

FIG. 2 is a block diagram depicting another exemplary embodiment ofphotonic device 101 configured to display the degenerate band edge. Thisembodiment is similar to the embodiment described with respect to FIG. 1except each layer 108 is omitted. In this case, anisotropic layers 106and 107 preferably have different thicknesses and/or differentpermittivity tensors

$\begin{matrix}{{ɛ_{A\; 1} = \begin{bmatrix}{ɛ_{1} + \delta_{1}} & 0 & 0 \\0 & {ɛ_{1} - \delta_{1}} & 0 \\0 & 0 & ɛ_{1{zz}}\end{bmatrix}},{ɛ_{A\; 2} = {\begin{bmatrix}{ɛ_{2} + {\delta_{2}\cos\; 2\varphi}} & {\delta_{2}\sin\; 2\varphi} & 0 \\{\delta_{2}\sin\; 2\varphi} & {ɛ_{2} - {\delta_{2}\cos\; 2\varphi}} & 0 \\0 & 0 & ɛ_{2{zz}}\end{bmatrix}.}}} & (7)\end{matrix}$Otherwise, the characteristics of this embodiment in FIG. 2 would bevery similar to that of the embodiment described with respect to FIG. 1.

FIGS. 3A-D are graphs depicting the k-ω diagram for the embodiment ofphotonic device 101 described with respect to FIG. 1 for four differentvalues of the thickness of the B layer 108, respectively. In the graphdepicted in FIG. 3B, the upper dispersion curve develops degenerate bandedge d described in (3) and associated with the frozen mode regime. (InFIG. 3B, the frequencies above band edge d can be referred to as thefrequency gap or photonic gap, while frequencies below band edge d canbe referred to as the frequency band or photonic band.) The embodimentof photonic device 101 described with respect to FIG. 1 can developdegenerate band edge d, provided that the misalignment angle φ betweenthe adjacent anisotropic layers 106 and 107 is different from 0 and π/2.If the physical parameters, such as the layer thicknesses and/or themisalignment angle φ, of photonic device 101 deviate from thosecorresponding to the situation depicted in FIG. 3B, the degenerate bandedge d turns into a regular band edge g described in (1) and depicted inFIGS. 3A, 3C and 3D. The k-ω diagram depicted in FIG. 3D corresponds tothe case where the B layers 108 are absent.

FIGS. 4A-C are schematic diagrams depicting a photonic device 101 duringthree stages of the frozen mode regime. Photonic device 101 shown hereis configured similar to that of the photonic device embodimentdescribed with respect to FIG. 1. Here, the frozen mode regime occursfor an incident electromagnetic pulse 102 with a central frequency closeto that of the degenerate band edge d depicted in FIG. 3B. FIG. 4Adepicts incident pulse 102 propagating towards the surface 111 ofphotonic device 101. FIG. 4B depicts the situation after pulse 102 hasreached surface 111 and has been transmitted into device 101 andconverted into the frozen mode pulse 401. Here, the frozen mode 401 ischaracterized by an enhanced pulse amplitude and compressed pulselength, compared to those of the incident pulse 102. FIG. 4C depicts thesituation after the frozen pulse 401 exits the photonic device 101 andturns into a reflected wave 402. The distance 404 through which thefrozen mode pulse 102 is transmitted inside photonic device 101, as wellthe degree of amplitude enhancement, are strongly dependent on the pulsebandwidth and the central frequency. The frozen mode amplitude willtypically increase with decreasing bandwidth and lesser differencebetween the central frequency and the degenerate band edge.

FIG. 5 is a graph depicting an exemplary smoothed frozen mode profile atthe steady-state frozen mode regime. In this example, the amplitude ofthe incident wave is unity. The point z=0 coincides with surface 111.

FIG. 6 is a graph depicting a smoothed profile of a typical surfaceelectromagnetic wave. Here, the field amplitude decays exponentiallywith the distance z from surface 111.

FIG. 7 is a graph depicting a smoothed profile of an exemplary abnormalsurface wave associated with the degenerate band edge (3) of theelectromagnetic spectrum. In this example, the field amplitude sharplyrises inside photonic device 101, before decaying as the distance z fromsurface 111 further increases. The magnitude and the location of thefield amplitude maximum sharply depend on the wave frequency.Remarkably, the maximal amplitude of an abnormal surface wave can bereached at a significant distance from surface 111. The lattercircumstance can suppress the energy leakage outside photonic device101.

FIG. 8 is a graph depicting a typical transmission dispersion ofphotonic device 101 with the k-ω diagram depicted in FIG. 3B. Here, N=16(in FIG. 8A) and N=32 (in FIG. 8B) is the total number of segments 105in device 101 and ω_(d) is the degenerate band edge frequency. The sharppeaks in the device transmittance correspond to giant cavity resonances,their exact position being dependent on the number N.

FIG. 9 is a graph depicting the smoothed field distribution A²(z) inphotonic device 101 at the frequency of the rightmost giant transmissionresonance closest to the degenerate band edge frequency ω_(d) depictedin FIG. 8, N=16 (in FIG. 9A) and N=32 (in FIG. 9B). The amplitude of theincident plane wave is unity, implying that the field enhancement in thecase N=16 reaches 2000, while in the case N=32, the filed enhancementreaches 35000. To achieve similar performance in a common periodic arrayof isotropic layers, one would generally need at least several hundredlayers in a stack.

FIG. 10 is a block diagram depicting another exemplary embodiment ofphotonic device 101. Here, device 101 is a spatially periodic structureconfigured to display an electromagnetic k-ω diagram with a degenerateband edge (3). In this embodiment, device 101 is configured as awaveguide with an X-Y cross-section periodically modulated along thewaveguide axis Z. In this embodiment, waveguide 101 includes a pluralityof segments (unit cells) 605 coupled together between a first end 603and a second end 604 of waveguide 101. Only the rightmost and theleftmost segments 605 are shown in FIG. 10. Each segment 605 has avariable cross-section depending on the coordinate Z, as shown in FIG.11. The end cross-sections 6051 and 6052 are identical, to ensure smoothconnection of adjacent segments 605 in the waveguide. At least at someZ, the X-Y cross-section of segment 605 is anisotropic in the X-Y plane.The term “anisotropic in the X-Y plane” implies that the axis Z of thewaveguide is not an n-fold symmetry axis of this particularcross-section with n>2. The length of each segment 605 in the Zdirection depends on operational frequency and is of the order of therespective electromagnetic wavelength.

In one exemplary embodiment, each segment 605 can be subdivided intothree adjacent portions 606-608, as depicted in FIG. 12 (portions606-608 are shown here spaced apart from each other, although this wouldnot be the case in the actual implementation). Portion 606 can be viewedas a circular section of the waveguide squeezed in the Y direction, sothat its cross-section in the middle has an elliptical shape, as seen inFIGS. 12 and 13A. Portion 607 in FIGS. 12 and 13B can be similar toportion 606, but rotated about the Z axis by an angle φ, preferablydifferent from 0 and π/2. In the embodiments depicted in FIGS. 10-13C,the misalignment angle φ is chosen π/4, although it is not limited tosuch. A third, optional portion 608, depicted in FIGS. 12 and 13C, canhave circular, or any other cross-section, or it can be omittedaltogether. The cross-sections at both ends of each of the threeportions 606-608 are identical to ensure their smooth interface in thewaveguide. In this example, the end cross-section is circular, althoughany desired shape can be used. One can view the shape anisotropy ofportions 606, 607, shown in FIGS. 12 and 13A-B, as being analogous tothe dielectric anisotropy (6) of the respective layers 106, 107 of theembodiment of the periodic layered structure 101 described with respectto FIG. 1. Portion 608 with a circular cross-section could be viewed asanalogous to isotropic layer 108 in FIG. 1.

Again, waveguide 101 as depicted in FIG. 10 can be configured to displaya degenerate band edge at desired frequency. By way of example, displayof the degenerate band edge can be done as follows: (i) by adjusting thevariable X-Y cross-section as a function of the axial coordinate Z, or(ii) by the proper choice of dielectric or other low-absorptionmaterials filling the waveguide. It should be noted that waveguide 101can display the electromagnetic band gap structure with a degenerateband edge in any manner and is not limited to just these two examples.

The input electromagnetic wave 602 enters waveguide 101 in FIG. 10 atend 603, similar to the embodiments described with respect to FIGS. 1-2.The optimal number of segments 605 in the device 601 can vary betweenthree and several hundred or more, depending on the specificapplication.

If this embodiment of waveguide 101 is empty, or if it is filled with auniform dielectric substance, the misaligned cross-section anisotropy ofportions 606 and 607 may become required for the existence of degenerateband edge. But if the filling material is not distributed uniformly, asshown in the exemplary embodiments of FIGS. 14-15C, the variablecross-section can also be circular, square, or any other.

FIGS. 14-15C depict another exemplary embodiment of photonic device 101as a waveguide configured to display the degenerate band edge in theelectromagnetic k-ω diagram. In this exemplary embodiment, the effect ofmisaligned cross-sectional anisotropy of waveguide 101 is achieved by anon-uniform filling of waveguide 101, rather than by anisotropy of theshape of the external X-Y cross-section. Here, the non-uniform fillingis provided by cylindrical insertions 710-711, although any manner ofnon-uniform filling can be used. In this embodiment with insertions710-711, there are no essential restrictions on the shape of the X-Ycross-section of waveguide 101, for example, it can be circular, square,or any other. In this embodiment, the cross-section shape is circularand independent of Z (i.e., there is no periodic external shapemodulation along the Z-direction, as in the exemplary embodimentsdescribed with respect to FIGS. 10-13). The photonic band gap structurein this case is created by a non-uniform filling (insertions 710-711) ofwaveguide 101. In FIG. 14, a single segment (unit cells) 705 ofwaveguide 101 is shown. The entire structure of waveguide 101 isobtained by repeating segment 705 in a periodic fashion along thewaveguide axis, similar to the embodiments described with respect toFIGS. 1, 2 and 10.

In the exemplary embodiment depicted in FIG. 14, a single segment (aunit cell) 705 includes three contiguous portions 706, 707, 708, shownalso separately in FIGS. 15A-C, respectively. One can view the role ofportions 706 and 707 as being analogous to that of the respective layers106 and 107 described with respect to FIG. 1, or portions 606 and 607described with respect to FIG. 12. Specifically, portions 706 and 707provide the misaligned structural anisotropy in the X-Y plane and,thereby, create the conditions for degenerate photonic band edge (3). Inthe embodiment depicted in FIG. 14, the anisotropy is created bymisaligned cylindrical insertions 710 and 711, each of which ispositioned in the center of the respective section and orientedperpendicular to the waveguide axis Z. The misalignment angle in the X-Yplane between insertions 710 and 711 is preferably different from 0 andπ/2. It can be set, for example, as π/4, as shown in FIG. 15B, or it canbe made variable to provide structural tunability. Portion 708 can beempty, or it can be filled with a uniform substance with low absorptionat operational frequency range, or it can be omitted altogether.Otherwise, the description of photonic device 101; one segment 105 ofwhich is depicted in FIG. 14, is similar to that in FIG. 10.

There can be a practically infinite number of specific waveguiderealizations of photonic device 101 displaying the degenerate band edge(3). In the embodiment in FIG. 10, the desired effect is achieved by themisaligned shape anisotropy of the waveguide cross-section. In theembodiment in FIG. 14, the same effect is achieved by non-uniformfilling of the waveguide. One can use any combination of these twoembodiments, or one can also exploit the misaligned dielectricanisotropy of a periodic stratified structure, as described with respectto FIGS. 1-2. In any event, the electromagnetic band gap structure(i.e., the k-ω diagram) of photonic device 101 can develop a degenerateband edge (3) and, thereby, display the frozen mode regime, only if theperiodic structure has the proper symmetry and possesses a certaindegree of complexity. The embodiments described with respect to FIGS.1-2 and 10-15C are only particular solutions or examples. One can useany combination of these embodiments or one can use other configurationsnot explicitly shown.

Described below are three exemplary methods in which photonic device 101can be used. Each of the methods is referred to as an independentregime. It should be noted that operation in any one regime is dependenton the needs of the specific application, and that these regimes do notconstitute an exhaustive list of potential uses for photonic device 101.In fact, photonic device 101 can be operated in any one or more of thesethree regimes as well as other regimes not explicitly described herein.

A first exemplary regime for photonic device 101 can be referred to asthe frozen mode regime at degenerate band edge frequency. In thisregime, an incident electromagnetic pulse 401 with central frequencyclose to that of the degenerate band edge is transmitted to photonicdevice 101, where it is converted into the frozen mode 402 havinggreatly enhanced amplitude and compressed length, similar to theexemplary embodiment described with respect to FIGS. 4A-C. Such a frozenmode does not propagate further through photonic device 101 thandistance 404, and after a certain delay pulse is reflected back tospace. During the time in which pulse 102 dwells inside photonic device101, its amplitude can exceed that of the incident wave in air byseveral orders of magnitude. FIG. 5, which was previously described,depicts the steady-state realization of the frozen mode regime. The factthat the frozen mode amplitude is drastically enhanced compared to thatof the incident wave can be used for enhancement of various processesresulting from light-matter interaction, for instance, higher harmonicgeneration, nonreciprocal Faraday rotation, light amplification byactive media, etc. The frozen mode regime at degenerate band edge isfundamentally different from that associated with stationary inflectionpoint and described in A. Figotin et al., U.S. Pat. No. 6,701,048.Indeed, in the case of stationary inflection point, the transmittedfrozen mode slowly propagates through the photonic device until itreaches its opposite boundary or gets absorbed by the medium. Bycontrast, in the case of the degenerate band edge described herein, theincident wave is eventually reflected back to space, as illustrated inFIG. 4C.

A second exemplary regime for photonic device 101 can be referred to asthe abnormal surface wave near degenerate band edge frequency regime. Inthe embodiments in FIGS. 1 and 2, the surface waves propagate alongsurface 111, normally to the Z direction. Typically, a surface waverapidly decays with the distance from surface 111 between the photoniccrystal and air, as depicted in FIG. 6. But, if the surface wavefrequency is close to that of a degenerate band edge, the surface waveprofile can change dramatically. The amplitude of such an abnormalsurface wave sharply increases with the distance Z from the interface,before it starts to decay, as depicted in FIG. 7. The abnormal surfacewave associated with degenerate band edge is much better confined insidephotonic device 101 reducing the energy leakage outside the system,because the leakage rate is usually proportional to the squared fieldamplitude A² at the slab/air interface 111. This regime of abnormalsurface wave is not exhibited in this precise manner in the exemplaryembodiments of FIGS. 10-15C using a waveguide setting.

A third exemplary regime for photonic device 101 can be referred to asgiant Fabry-Perot cavity resonance near the degenerate band edgefrequency. Periodically modulated waveguides, periodic layeredstructures, as well as periodic arrays with 2 and 3 dimensionalperiodicity terminated by plane-parallel boundaries, are known todisplay sharp transmission cavity resonances at frequencies close to aphotonic band edge. This phenomenon has been widely used in resonancecavities for varies practical purposes. In the case of a regularphotonic band edge (1), the amplitude A of the resonance field insidethe photonic cavity can be estimated asA∝NA₀  (4)where A₀ is the amplitude of the incident plane wave. Strong cavityresonance can require a large number N of unit cells (e.g., segments105, 605 and 705) in the periodic structure. A similar resonance effectoccurs in periodic structures in the vicinity of the degenerate photonicband edge (3), as depicted in FIG. 8. One difference though is that inthe latter case, the resonance field amplitude is estimated asA∝N²A₀  (5)and referred to as the giant transmission band edge resonance. Thisshows that a Fabry-Perot cavity based on photonic device 101 configuredto display the degenerate band edge is much more efficient than previousversions. For instance, a resonance cavity with the degenerate band edgebased on an exemplary embodiment of device 101 having 10 periodicsegments (e.g, 105, 605 or 705), or unit cells, can perform as well as aregular Fabry-Perot photonic cavity composed of 100 periodic segments.The optimal number of segments (e.g, 105, 605 or 705) in the resonancecavity depends on specific application, but in any event, cavities basedon photonic device 101 configured to display the degenerate band edgecan be much smaller.

The embodiments described with respect to FIGS. 1-15C provide numerousadvantages over conventional systems and devices. For instance, photonicdevice 101 does not have to include any magnetic components with strongFaraday rotation, as is the case in the devices described in A. Figotinet al., U.S. Pat. No. 6,701,048, entitled “Unidirectional GyrotropicPhotonic Crystal and Applications for the Same,” which is fullyincorporated by reference herein. Also, photonic device 101 can operatewithout the inclusion of layers with an oblique orientation of theanisotropy axis relative to the normal to the layers, similar to certaindevices described in A. Figotin et al., U.S. patent application Ser. No.10/839,117, filed May 3, 2004 and entitled “Systems and Methods forTransmitting Electromagnetic Energy in a Photonic Device,” which is alsofully incorporated by reference herein. In addition, the regime of thegiant transmission resonance described above can be realized exclusivelyin the photonic devices configured to display degenerate photonic bandedge (3). Additional information relating to photonic devices 101configured to display degenerate band edges is contained in A. Figotinet al., “Gigantic Transmission Band-Edge Resonance in Periodic Stacks ofAnisotropic Layers,” Physical Review E 72, 036619, published Sep. 29,2005, which is also fully incorporated by reference herein.

Photonic device 101 can be incorporated in numerous photonic systemsimplemented in a myriad of applications. For instance, photonic device101 can be implemented as a tunable delay line, an efficient nonlinearelement used for frequency conversion, wave mixing and the like, it canalso be used as a high performance resonance cavity in an opticalamplifier and in a laser, a host for a multi-dimensional opticalnetwork, an incident wave receiver and the like. It should be noted thatthese examples are not intended to limit, in any way, the systems andmethods in which photonic device 101 can be used. Nor are these examplesintended to limit photonic device 101 to any one type of system,application or technology.

In the foregoing specification, the invention has been described withreference to specific embodiments thereof. It will, however, be evidentthat various modifications and changes may be made thereto withoutdeparting from the broader spirit and scope of the invention. Forexample, the reader is to understand that the specific ordering andcombination of process actions shown in the process flow diagramsdescribed herein is merely illustrative, unless otherwise stated, andthe invention can be performed using different or additional processactions, or a different combination or ordering of process actions. Asanother example, each feature of one embodiment can be mixed and matchedwith other features shown in other embodiments. Features and processesknown to those of ordinary skill may similarly be incorporated asdesired. Additionally and obviously, features may be added or subtractedas desired. Accordingly, the invention is not to be restricted except inlight of the attached claims and their equivalents.

1. A photonic device, comprising: a periodic structure having anelectromagnetic dispersion relation that exhibits a frequency gap with adegenerate band edge for an input electromagnetic wave propagating in afirst direction, wherein the structure is periodic in the firstdirection, wherein the structure is configured as an electromagneticwaveguide comprising a plurality of periodic segments and wherein thefirst direction is a Z direction and each segment has a variablecross-sectional shape measured along a X-Y plane formed by an Xdirection and a Y direction, the X direction being perpendicular to theZ direction and the Y direction being perpendicular to the X and Zdirections.
 2. The photonic device of claim 1, wherein the structure isa fiber configured to operate over a frequency range in the opticalportion of the electromagnetic spectrum.
 3. The photonic device of claim1, wherein the cross-sectional shape of at least a portion of eachsegment is anisotropic in the X-Y plane.
 4. A photonic device,comprising: a periodic structure having an electromagnetic dispersionrelation that exhibits a frequency gap with a degenerate band edge foran input electromagnetic wave propagating in a first direction, whereinthe structure is periodic in the first direction, wherein the structureis configured as an electromagnetic waveguide comprising a plurality ofperiodic segments and wherein each of the segments comprises a firstportion and a second portion located successively along the firstdirection, the first portion comprising a first non-uniform material andthe second portion comprising a second non-uniform material, wherein thefirst portion has an anisotropy in the X-Y plane misaligned from ananisotropy of the second portion.
 5. The photonic device of claim 4,wherein each of the segments comprises a third isotropic in the X-Yplane portion.